DocumentCode
3328282
Title
Velocity magnitude control of maneuverable reentry warhead
Author
Kaifeng Liu ; Xinxue Liu ; Fang Wang ; Jian Wu
Author_Institution
Xi´an Res. Inst. of High-tech, Xi´an, China
Volume
1
fYear
2011
fDate
22-24 Aug. 2011
Firstpage
374
Lastpage
377
Abstract
In this paper, the kinematic model of reentry warhead was built to verify the effect of control law. Then, an idea velocity curve was designed to support a standard of velocity control and the calculation of attack angle and sideslip angle was discussed. Finally, the efficiency of control law was verified through simulation. The simulation result shows that the control law proposed in this paper can limit the velocity magnitude error within 10m without losing accuracy of control of fall point and velocity direction.
Keywords
military systems; velocity control; weapons; attack angle; kinematic model; maneuverable reentry warhead; reentry warhead; velocity control; velocity curve; velocity magnitude control; ideal velocity curve; reentry maneuverable warhead; supplementary attack angle; velocity magnitude control;
fLanguage
English
Publisher
ieee
Conference_Titel
Strategic Technology (IFOST), 2011 6th International Forum on
Conference_Location
Harbin, Heilongjiang
Print_ISBN
978-1-4577-0398-0
Type
conf
DOI
10.1109/IFOST.2011.6021043
Filename
6021043
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